Chromizing over cathodic arc coating

a technology of cathodic arc and coating, applied in the direction of solid-state diffusion coating, superimposed coating process, machines/engines, etc., can solve the problems of significant loss of coating thickness, constant threat to the hardware of such machinery, e.g., turbine blades,

Active Publication Date: 2019-07-30
RTX CORP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The chromium-rich cathodic arc coating provides superior hot corrosion resistance without the costs and thickness losses associated with conventional methods, maintaining performance across a wide temperature range and resisting stress corrosion and low cycle fatigue.

Problems solved by technology

The hardware of such machinery, e.g., a turbine blade, is continuously threatened by extreme hot corrosion.
Nevertheless, the conventional combined coating process requires considerable additional cost and causes significant loss in coating thickness due to aggressive grit blast and spallation.

Method used

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  • Chromizing over cathodic arc coating
  • Chromizing over cathodic arc coating
  • Chromizing over cathodic arc coating

Examples

Experimental program
Comparison scheme
Effect test

example 1

to Produce Coating Specimens

[0072]The processes to deposit the various coating specimens in the present application are summarized in Table 1.

[0073]

TABLE 1Definition of the processes to deposit the coatings specimensOperationscathodiccoatingarcdiffusionheavycathodicspecimencoatingDHTpeeningcoatinggrit blastarc coatingDHTpeeningMCrAIY123MCrAIY / 12345diffusedchromidecoatingdiffused1234chromidecoating / MCrAIY(FP)diffused12chromidecoating / MCrAIY(NP)

[0074]A conventional cathodic arc coating MCrAlY is used as a baseline in the hot corrosion and LCF tests.

[0075]The coating specimen MCrAlY / Diffused chromide coating is processed by the conventional method by depositing sequentially a diffusion coating, heavy grip blast to remove the coating surface, and a cathodic arc coating, followed by DHT and peening operation. The MCrAlY / Diffused chromide coating specimen is also used as a baseline in the hot corrosion and LCF tests.

[0076]The coating specimen diffused chromide coating / MCrAlY (FP) and the ...

example 2

of Chromizing Over Cathodic Arc Coating

[0077]FIG. 2 shows optical microscopic views of each coating specimen.

[0078]Nominal coating thicknesses are between about 2.5 mil and 3 mil.

[0079]MCrAlY and MCrAlY / diffused chromide coating specimens are observed to have consistent microstructures as previously predicted.

[0080]In contrast, diffused chromide coating / MCrAlY (FP) and diffused chromide coating / MCrAlY (NP) specimen coatings contain oxides / nitrides inclusions. The majority of these coatings was found to be single phase, likely 7-Ni FCC solid solution, due to Cr enrichment resulting from the diffusion coating deposition. Angular Al-rich phases, like nitrides, resulting from the diffusion coating process, are visible in these coatings as well.

[0081]As shown in the SEM image and associated Cr x-ray map in FIG. 3, the deposition of diffused chromide coating atop MCrAlY on a scrap blade results in the formation of a nearly continuous highly elevated Cr-rich phase at the surface.

example 3

Fatigue (LCF) Test Result

[0082]LCF tests were performed with the coating specimens at the temperature of 1200° F.

[0083]FIG. 4 shows a plot of maximum stress value vs. cycles to failure for each LCF testing. R value for this plot is 0.5.

[0084]Maximum stress value for each specimen was investigated within the range of 120 ksi˜140 ksi. At a maximum stress of 120 ksi, no significant differences were observed between each coating specimen; failure generally occurred at approximately 100,000 cycles. At 140 ksi maximum stress, MCrAlY and MCrAlY / diffused chromide coating specimens failed within the first 100 cycles. diffused chromide coating / MCrAlY (FP) and diffused chromide coating / MCrAlY (NP) specimens failed at greater than 1000 cycles. There is no distinction between the test results of diffused chromide coating / MCrAlY (FP) and diffused chromide coating / MCrAlY (NP).

[0085]In conclusion, there is no indication that LCF resistance is associated with the preparation process, e.g., DHT and p...

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Abstract

The present invention provides a Cr-rich cathodic arc coating, an article in turbine blade coated with the chromizing over cathodic arc coating, and a method to produce the coating thereof. The Cr-rich cathodic arc coating in the present invention comprises a cathodic arc coating and a diffusion coating deposited atop the cathodic arc coating to enforce hot corrosion resistance. The hardware coated with the chromizing over cathodic arc coating in the present invention is reinforced with superior-hot corrosion resistance. The present invention further provides a novel method for producing the chromizing over cathodic arc coating by re-sequencing coating deposition order. The method in the present invention is efficient and cost-reducing by eliminating some operations, e.g., DHT and peening, between the cathodic arc coating and the diffusion coating. The hot corrosion resistance in the present invention results from the high Cr content in the surface of the coating.

Description

RELATED APPLICATIONS[0001]This application is a National Phase Application of Patent Application PCT / 2014 / 066277 filed on Nov. 19, 2014, which claims the benefit of and priority to U.S. Provisional Patent Application No. 61 / 914,222, filed Dec. 10, 2013, the contents each of which are incorporated herein by reference in their entirety.FIELD OF THE INVENTION[0002]This invention relates to a Cr-rich cathodic arc coating which provides superior hot corrosion resistance, an article with such Cr-rich cathodic arc coating, and a method to produce the Cr-rich cathodic arc coating by re-sequencing coating deposition order.BACKGROUND[0003]High-temperature corrosion (hot corrosion) is a mechanism of corrosion that takes place in gas turbines, diesel engines, furnaces or other machinery coming in contact with hot gas containing certain contaminants. The hardware of such machinery, e.g., a turbine blade, is continuously threatened by extreme hot corrosion. In such region of gas turbines or engin...

Claims

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Application Information

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Patent Type & AuthorityPatents(United States)
IPC IPC(8): C23C14/58C23C10/10B32B15/04C23C10/32C23C14/14C23C30/00C23C14/34F01D5/28C23C10/38C23C14/16C23C28/02C23C10/20
CPCC23C14/5846B32B15/043C23C10/10C23C10/20C23C10/32C23C10/38C23C14/14C23C14/16C23C14/34C23C14/3464C23C14/5806C23C28/02C23C28/021C23C28/022C23C30/00C23C30/005F01D5/28F01D5/288B32B15/04Y10T428/12979F05D2220/32F05D2230/90F05D2300/177F05D2300/611Y10T428/12847Y10T428/12854Y10T428/12931Y10T428/12937
InventorTRZCINSKI, FRANK J.BALZANO, THOMASSINESI, PRENTICE M.LIVINGS, MARK A.TASK, MICHAEL N.
OwnerRTX CORP